NUSAT-53 (JANE GOODALL), 68432
Orbit data source: Space-Track
NUSAT-53 (JANE GOODALL), 68432 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68432 intel report (Beta)
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Identifier
Orbit
Country
AR / ARGNRelated business
Manufacturer
URUGUS S.A.
Mission
Operational Commercial Imaging
Bus & Motor
NEWSAT V, Unknown motor
Mass
41.5 kg wet, 38.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 NUSAT-53 (JANE GOODALL)
1 68432U 26067S 26219.85170254 .00002725 00000-0 13342-3 0 9998
2 68432 97.4589 177.6674 0002585 151.6167 208.5208 15.19022448 19788Epoch: 2026-08-07T20:26Z
TLE epoch observation values (Epoch: 2026-08-07T20:26:27.099Z)
Latitude
-0.00009°
Longitude
-85.31696°
Altitude
513.446 km
Speed
7.606 km/s
True Right ascension
11h 50m 40s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:47:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.543 km
Perigee altitude
503.984 km
Semi-major axis
6,883.9 km
Eccentricity
0.00026
Inclination
97.4589°
RAAN
177.6674°
Arg. of periapsis
151.6167°
True anomaly
208.50666°
Mean anomaly
208.5208°
Eccentric anomaly
208.51373°
Mean motion
3.80007 °/min
Orbital period
94.74 mins
BSTAR
0.00013342
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NUSAT-53 (JANE GOODALL) Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-08 09:39:57.434Z | 38.118° NE | 2026-08-08 09:41:57.434Z | 82.726° E | 29.989° | 2026-08-08 09:44:57.434Z | 160.327° S |
| 4 mins | 2026-08-08 21:52:57.434Z | 220.365° SW | 2026-08-08 21:54:57.434Z | 278.549° WNW | 26.516° | 2026-08-08 21:56:57.434Z | 319.094° NNW |
| 4 mins | 2026-08-09 09:23:57.434Z | 64.213° ENE | 2026-08-09 09:24:57.434Z | 86.397° E | 20.651° | 2026-08-09 09:27:57.434Z | 145.506° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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